High pressure gas sealing
View Patent ↗A gas processing system includes a vessel defining a cavity for processing a gas. The vessel includes a process gas inlet for accepting process gas at an input pressure, and a process gas outlet for discharging process gas at an output pressure. The gas processing system further includes a shaft coupled to the vessel and a multistage sealing system comprising multiple seals spaced along the shaft. The shaft is configured to transfer mechanical energy to or from gas in the vessel. Each adjacent pair of seals defines a corresponding pressure space therebetween. One of the pressure spaces is an equalizing pressure space in hydraulic communication with the process gas inlet via a flow line, such that in operation, pressure in the equalizing pressure space is maintained at an equalized pressure with respect to a pressure in the process gas inlet.
1. A gas compressor system comprising:
a compressor cylinder defining a cavity for processing a gas and comprising a compressor cylinder gas inlet for accepting process gas into the cavity at an input pressure, and a compressor cylinder gas outlet for discharging process gas from the cavity at an output pressure that is higher than the input pressure;
a reciprocating shaft coupled to the compressor cylinder and configured to transfer mechanical energy to gas in the compressor cylinder; and
a progressive sealing system that defines an intermediate pressure space between adjacent seals spaced along the reciprocating shaft between the cavity and atmosphere,
wherein the intermediate pressure space is in fluid communication with the compressor cylinder gas inlet via a flow line spaced from the reciprocating shaft such that process gas leaked from the compression cylinder into the intermediate pressure space is ported back to the compressor cylinder gas inlet.
2. The gas compressor system of claim 1 , wherein the sealing system defines multiple pressure spaces between adjacent seals spaced along the shaft, including the intermediate pressure space and a second space that in operation reaches a maximum pressure lower than a maximum pressure in the intermediate pressure space and higher than atmospheric pressure.
3. The gas compressor system of claim 2 , further comprising a purge gas source in fluid communication with the second pressure space and under sufficient pressure to cause purge gas to flow from the purge gas source into the sealing system and along the shaft away from the vessel.
4. The gas compressor system of claim 3 , wherein the multiple pressure spaces include a vent pressure space in fluid communication with a vent for venting at least some of the purge gas.
5. The gas compressor system of claim 2 , wherein the sealing system comprises a series of four seals defining three pressure spaces.
6. The gas compressor system of claim 5 , wherein the multiple pressure spaces include a pressure space in fluid communication with a pressurized source of lubricant.
7. The gas compressor system of claim 1 , wherein the intermediate pressure space is in direct fluid communication with the process gas inlet.
8. The gas compressor system of claim 1 , wherein the shaft rotates with respect to the vessel during transfer of energy between the shaft and process gas within the vessel, the shaft rotating within the sealing system.
9. The gas compressor system of claim 1 , wherein each of the seals is mounted in a respective one of a plurality of seal housings coupled together along the shaft.
10. The gas compressor system of claim 1 , configured such that in operation, pressure in the intermediate pressure space is maintained within 30 percent of the input pressure.
11. The gas compressor system of claim 1 , wherein the flow line is the only inlet or outlet into or out of the intermediate pressure space in operation, other than along a surface of the reciprocating shaft.
12. The gas compressor system of claim 1 , wherein the adjacent seals are adjacent portions of a continuous labyrinth seal, the intermediate pressure space being an intermediate portion of a labyrinth flow path through the seal.
13. The gas compressor system of claim 1 , wherein the flow path defines a throttling orifice.
14. The gas compressor system of claim 13 , wherein the throttling orifice is adjustable and/or controllable.
15. The gas compressor system of claim 1 , wherein the flow path defines a one-way valve that restricts flow along the flow path toward the intermediate pressure space.
16. The gas compressor system of claim 1 , wherein each of the seals is mounted in a respective one of a plurality of seal housings coupled together along the reciprocating shaft.
17. The gas compressor system of claim 1 , wherein the flow line is defined in part by aligned apertures in multiple seal housings.
18. The gas compressor system of claim 1 , wherein the compressor cylinder, the reciprocating shaft and the sealing system are components of a first gas compression stage, the gas compressor system further comprising a second gas compression stage having a second compressor cylinder, a second shaft and a second multistage sealing system, the first and second gas compression stages connected such that the output of the first gas compression stage is connected to an input of the second gas compression stage, and wherein the second multistage sealing system defines a second intermediate pressure space in fluid communication with the compressor cylinder gas inlet of the compressor cylinder of the first gas compression stage via a second flow line.